| タイトル | Adapting the SpaceCube v2.0 Data Processing System for Mission-Unique Application Requirements |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150011026 |
| 著者（英） | Sparacino, Pietro; Petrick, David; Hasouneh, Munther; Thomas, Luke; Stone, Robert; Winternitz, Luke; Gill, Nat; Flatley, Thomas; Davis, Milton |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2015-06-15 |
| 言語 | eng |
| 内容記述 | The SpaceCube (sup TM) v2.0 system is a superior high performance, reconfigurable, hybrid data processing system that can be used in a multitude of applications including those that require a radiation hardened and reliable solution. This paper provides an overview of the design architecture, flexibility, and the advantages of the modular SpaceCube v2.0 high performance data processing system for space applications. The current state of the proven SpaceCube technology is based on nine years of engineering and operations. Five systems have been successfully operated in space starting in 2008 with four more to be delivered for launch vehicle integration in 2015. The SpaceCube v2.0 system is also baselined as the avionics solution for five additional flight projects and is always a top consideration as the core avionics for new instruments or spacecraft control. This paper will highlight how this multipurpose system is currently being used to solve design challenges of three independent applications. The SpaceCube hardware adapts to new system requirements by allowing for application-unique interface cards that are utilized by reconfiguring the underlying programmable elements on the core processor card. We will show how this system is being used to improve on a heritage NASA GPS technology, enable a cutting-edge LiDAR instrument, and serve as a typical command and data handling (C&DH) computer for a space robotics technology demonstration. |
| NASA分類 | Communications and Radar; Avionics and Aircraft Instrumentation; Electronics and Electrical Engineering |
| レポートNO | GSFC-E-DAA-TN23515 |
| 権利 | No Copyright |
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